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Airworthiness Directives; Bell Helicopter Textron Canada (BHTC) Model 222, 222B, 222U, and 230 Helicopters

airworthiness · Rule · Final rule. · Published 2000-05-22 · 65 FR 32021

Document

Document number
00-12818
Federal Register citation
65 FR 32021
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2000-05-22
FAA docket
Docket No. 99-SW-43-AD

Abstract

This amendment adopts a new airworthiness directive (AD) for BHTC Model 222, 222B, 222U, and 230 helicopters that requires inspecting each flapping bearing to yoke attachment bolt (bolt) and replacing each bolt that shows thread damage, shank wear, or corrosion pitting with an airworthy bolt. This amendment is prompted by the discovery of a fractured bolt during a post-flight inspection. The actions specified by this AD are intended to prevent a fracture of a bolt, failure of the bearing and yoke interface, and subsequent loss of control of the helicopter.

Source

Authoritative
Federal Register document
Machine
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